TY - JOUR
T1 - Forecasting-based data-driven model-free adaptive sliding mode attitude control of combined spacecraft
AU - Gao, Han
AU - Ma, Guangfu
AU - Lv, Yueyong
AU - Guo, Yanning
N1 - Publisher Copyright:
© 2019 Elsevier Masson SAS
PY - 2019/3
Y1 - 2019/3
N2 - In this paper, a novel forecasting-based data-driven model-free adaptive sliding mode attitude control (FMFASMC) method is proposed for the postcapture combined spacecraft in the presence of unknown mathematical model and external disturbance. First, a forecasting-based data-driven model-free adaptive controller (FMFAC) is developed to ensure its adaptation to various working conditions by simultaneous adjustment of controller parameters with online and offline input–output measurement data. Then, a sliding-mode-based supplementary controller is introduced to improve the tracking performance of FMFAC in terms of robustness. Compared with existing works, the designed control scheme only utilizes the attitude angle and attitude angular velocity of the combined spacecraft, not requiring corresponding mechanism model, thereby dramatically curtailing the complexity and difficulty of relevant controller design. Finally, simulation comparisons between the FMFASMC, FMFAC, and traditional model-free adaptive control (MFAC) are presented for two groups of illustrative examples. The simulation results verify the effectiveness of the proposed control method.
AB - In this paper, a novel forecasting-based data-driven model-free adaptive sliding mode attitude control (FMFASMC) method is proposed for the postcapture combined spacecraft in the presence of unknown mathematical model and external disturbance. First, a forecasting-based data-driven model-free adaptive controller (FMFAC) is developed to ensure its adaptation to various working conditions by simultaneous adjustment of controller parameters with online and offline input–output measurement data. Then, a sliding-mode-based supplementary controller is introduced to improve the tracking performance of FMFAC in terms of robustness. Compared with existing works, the designed control scheme only utilizes the attitude angle and attitude angular velocity of the combined spacecraft, not requiring corresponding mechanism model, thereby dramatically curtailing the complexity and difficulty of relevant controller design. Finally, simulation comparisons between the FMFASMC, FMFAC, and traditional model-free adaptive control (MFAC) are presented for two groups of illustrative examples. The simulation results verify the effectiveness of the proposed control method.
KW - Combined spacecraft
KW - Data-driven control
KW - Supplementary control
UR - https://www.scopus.com/pages/publications/85060581643
U2 - 10.1016/j.ast.2019.01.004
DO - 10.1016/j.ast.2019.01.004
M3 - Article
AN - SCOPUS:85060581643
SN - 1270-9638
VL - 86
SP - 364
EP - 374
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
ER -